Aerospace
 Engineering



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First generation of the Aviation group professors at Technical Faculty in Belgrade (1937/38) <br>First row, left to right: eng. Nikola Obradović, eng. Dušan Tomić, dr. eng. Miroslav Nenadović <br>Second row, left to right: eng. Dušan Stankov, eng Milan Pajević, eng. lt. col. Dušan Lučić, eng. Slobodan Dobrosavljević, eng. Sima Milutinović
Wind Tunnel SB-1 (now „Miroslav Nenadović“) was one of the largest Prandtl type wind tunnels for educational purposes in the world after its construction was completed (1956) with the dimensions of the working section 2.90 x 2.10 x 6.0 m (up left: WT building, up right: 3D model of WT, down left: Working section, down right: WT power plant fan)
Historical review of tests in the wind tunnel „Miroslav Nenadović“ (up left: Avala TV tower testing, up right: Modified airfoil GAW testing, down left: Tomos GP motorcycle testing, down right: Thermal Power Plant Kolubara B cooling towers testing)
Recent tests in the wind tunnel „Miroslav Nenadović“ (up left: Testing of the optoelectronics system, up right: Students competition airfoil design, down left: Small HAWT testing, down right: Small VAWT testing)
Static testing laboratory (hangar) with ultra heavy duty floor (up to 60 tons/m<sup>2</sup>) equiped with hydraulic power unit (up left: Hangar building, down left: Hydraulic power unit control interface, right: General aviation aircraft wing bending test)
Static and dynamic testing of helicopter and wind turbine blades
Production of wind turbine and helicopter blades
Design of a general aviation class airplane (length 7.44 m, height 2.99 m, span 9.8 m)
Light helicopter design: two passangers, 2 x 125 hp engine, two-blade main rotor, composite cabin construction, aluminium motor compartment, tail boom and landing gear (up left: Light helicopter model, up right: Main rotor hub and blade design and manufacture, down left: Main gearbox design and manufacture, down right: Cabin compartment design and manufacture)
Propulsion systems design (up left: 8 hp engine for the UAV, up right: 6 hp engine for the UAV, down left: 54 hp engine for the UAV, down right: Micro turbojet engine TMM40)
PIV system in the wind tunnel
GOM-ARAMIS Digital Image Correlation system with high speed cameras
Aircraft inspection and forensics
CFD analysis
Finite element analysis
Rapid prototyping
Student’s association Beoavia
Current teaching staff of the Department of Aerospace Engineering at the Faculty of Mechanical Engineering in Belgrade (2021/22)